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15.1 Fluid Density, Specific Gravity, and Viscosity Correlations

Key Takeaways

  • Saturated liquid density is accurately estimated using the Rackett equation V_sat = (R * T_c / P_c) * Z_RA^[1 + (1 - T_r)^(2/7)], providing molar volume within 1-2% error up to reduced temperatures of T_r ≈ 0.95.

  • Specific gravity (SG) compares liquid density to pure water at 4°C (1,000 kg/m³ or 62.43 lbm/ft³) or 60°F (62.37 lbm/ft³); API gravity (°API = 141.5 / SG_60/60F - 131.5) scales inversely with density, where higher °API signifies a lighter, lower-density hydrocarbon.

  • Dynamic (absolute) viscosity μ (cP, Pa·s, lbm/(ft·s)) and kinematic viscosity ν = μ / ρ (cSt, m²/s, ft²/s) must never be confused: 1 cP = 10⁻³ Pa·s = 6.7197 × 10⁻⁴ lbm/(ft·s) and 1 cSt = 10⁻⁶ m²/s = 1.0764 × 10⁻⁵ ft²/s.

  • Non-Newtonian fluid behaviors diverge from Newton's linear law: pseudoplastics (shear-thinning, n < 1) exhibit decreasing apparent viscosity μ_app = K * (γ_dot)^(n-1) with shear rate, dilatants (shear-thickening, n > 1) exhibit increasing viscosity, and Bingham plastics require exceeding a yield stress τ_0 to initiate flow.

  • Temperature effects on viscosity are diametrically opposed between phases: liquid viscosity decreases exponentially with temperature via Andrade's relation ln(μ) = A + B/T due to thermal expansion weakening intermolecular cohesive forces, whereas gas viscosity increases with temperature (μ ∝ T^(1/2) or Sutherland's formula) due to increased molecular collision frequency.

Last updated: September 2026

15.1 Fluid Density, Specific Gravity, and Viscosity Correlations

Accurate evaluation of fluid density and viscosity is essential for solving core chemical engineering problems on the NCEES PE Chemical Exam, including line sizing, pump and compressor power calculations, frictional head loss determination via the Moody diagram, and boundary layer transport analysis. Chemical process streams span pure solvents, cryogenic liquefied gases, heavy crude oils, non-Newtonian polymer melts, and high-pressure supercritical gases.


1. Fluid Density and Specific Gravity Formulations

Mass Density, Specific Volume, and Specific Gravity

Mass density (ρ\rho) is defined as mass per unit volume (kg/m3\text{kg/m}^3 or lbm/ft3\text{lbm/ft}^3). Its reciprocal is specific volume (v=1/ρv = 1/\rho, with units m3/kg\text{m}^3/\text{kg} or ft3/lbm\text{ft}^3/\text{lbm}). On a molar basis, molar density is ρm=ρ/M\rho_m = \rho / M and molar volume is V=M/ρV = M / \rho, where MM is the molecular weight.

Specific gravity (SGSG) is a dimensionless ratio comparing the density of a target fluid to the density of a standard reference fluid at specified reference temperatures:

SG=ρfluid(T)ρref(Tref)SG = \frac{\rho_{\text{fluid}}(T)}{\rho_{\text{ref}}(T_{\text{ref}})}
  • Liquids (Standard Reference): Pure liquid water at its maximum density point (4.0∘C4.0^\circ\text{C} or 39.2∘F39.2^\circ\text{F} and 1.0 atm1.0\text{ atm}): ρwater(4∘C)=1000.0 kg/m3=1.0000 g/cm3=62.428 lbm/ft3=8.3454 lb/gal\rho_{\text{water}}(4^\circ\text{C}) = 1000.0\text{ kg/m}^3 = 1.0000\text{ g/cm}^3 = 62.428\text{ lbm/ft}^3 = 8.3454\text{ lb/gal}
  • Petroleum Industry Standard (SG60/60∘FSG_{60/60^\circ\text{F}}): In petroleum refining and custody transfer, specific gravity is evaluated at 60.0∘F60.0^\circ\text{F} (15.56∘C15.56^\circ\text{C}) relative to water at 60.0∘F60.0^\circ\text{F}: ρwater(60∘F)=999.01 kg/m3=62.366 lbm/ft3=8.3371 lb/gal\rho_{\text{water}}(60^\circ\text{F}) = 999.01\text{ kg/m}^3 = 62.366\text{ lbm/ft}^3 = 8.3371\text{ lb/gal}
  • Gases (Standard Reference): Dry air at 0∘C0^\circ\text{C} (32∘F32^\circ\text{F}) or 60∘F60^\circ\text{F} and 1.0 atm1.0\text{ atm} (Mair=28.964 kg/kmolM_{\text{air}} = 28.964\text{ kg/kmol} or lbm/lbmol\text{lbm/lbmol}): SGgas=MgasMairSG_{\text{gas}} = \frac{M_{\text{gas}}}{M_{\text{air}}}

API Gravity (∘API^\circ\text{API}) and Baumé Scales (∘Beˊ^\circ\text{Bé})

In petroleum refining, the American Petroleum Institute defined the API Gravity scale to characterize crude fractions:

∘API=141.5SG60/60∘F−131.5  ⟺  SG60/60∘F=141.5∘API+131.5^\circ\text{API} = \frac{141.5}{SG_{60/60^\circ\text{F}}} - 131.5 \iff SG_{60/60^\circ\text{F}} = \frac{141.5}{^\circ\text{API} + 131.5}

Notice the strict inverse mathematical relationship: as fluid density increases, API gravity decreases.

  • Water (SG=1.000SG = 1.000) corresponds exactly to 10.0∘API10.0^\circ\text{API}.
  • Light crudes (>31.1∘API> 31.1^\circ\text{API}) have SG<0.870SG < 0.870 (e.g., gasoline ≈60∘API\approx 60^\circ\text{API}, kerosene ≈42∘API\approx 42^\circ\text{API}).
  • Heavy crudes (<22.3∘API< 22.3^\circ\text{API}) have SG>0.920SG > 0.920.
  • Bitumen and extra-heavy oils have ∘API<10.0∘^\circ\text{API} < 10.0^\circ, meaning SG>1.000SG > 1.000, causing them to sink in water.

For inorganic aqueous process solutions (e.g., sulfuric acid, caustic soda, brine), the Baumé scale (∘Beˊ^\circ\text{Bé}) is utilized:

For liquids heavier than water (SG>1.0):∘Beˊ=145−145SG60/60∘F  ⟺  SG=145145−∘Beˊ\text{For liquids heavier than water } (SG > 1.0): \quad ^\circ\text{Bé} = 145 - \frac{145}{SG_{60/60^\circ\text{F}}} \iff SG = \frac{145}{145 - ^\circ\text{Bé}} For liquids lighter than water (SG<1.0):∘Beˊ=140SG60/60∘F−130  ⟺  SG=140130+∘Beˊ\text{For liquids lighter than water } (SG < 1.0): \quad ^\circ\text{Bé} = \frac{140}{SG_{60/60^\circ\text{F}}} - 130 \iff SG = \frac{140}{130 + ^\circ\text{Bé}}

Saturated Liquid Density: The Rackett Equation

For saturated pure liquids, the Rackett equation provides high-precision estimates of molar volume from the triple point up to reduced temperatures of Tr≈0.95T_r \approx 0.95:

Vsat=RTcPcZRA[1+(1−Tr)2/7]V_{\text{sat}} = \frac{R T_c}{P_c} Z_{RA}^{\left[ 1 + (1 - T_r)^{2/7} \right]}

Where:

  • VsatV_{\text{sat}} = saturated liquid molar volume (m3/kmol\text{m}^3/\text{kmol} or cm3/mol\text{cm}^3/\text{mol}).
  • Tc,PcT_c, P_c = critical temperature (K\text{K}) and critical pressure (kPa\text{kPa} or bar\text{bar}).
  • Tr=T/TcT_r = T / T_c = reduced temperature.
  • ZRAZ_{RA} = pure-component Rackett compressibility parameter (tabulated in the NCEES PE Chemical Reference Handbook; if unavailable, approximate with critical compressibility factor Zc=PcVc/(RTc)Z_c = P_c V_c / (R T_c)).
  • RR = universal gas constant (8.3145 kPa⋅m3/(kmol⋅K)8.3145\text{ kPa}\cdot\text{m}^3/(\text{kmol}\cdot\text{K})).

The saturated liquid mass density is calculated directly from the molar volume:

ρsat=MVsat\rho_{\text{sat}} = \frac{M}{V_{\text{sat}}}

Ideal and Real Gas Density

Gas density is calculated using the equation of state:

ρgas=PMZRT\rho_{\text{gas}} = \frac{P M}{Z R T}

Where ZZ is the compressibility factor (Z=1.0Z = 1.0 for ideal gases). For real gases at elevated pressures, ZZ is obtained from generalized compressibility charts using reduced properties (Tr=T/Tc,Pr=P/PcT_r = T/T_c, P_r = P/P_c) or cubic equations of state (Peng-Robinson, SRK).


2. Viscosity Fundamentals: Dynamic vs. Kinematic

Newton's Law of Viscosity

Viscosity quantifies internal resistance to shear-induced deformation. In laminar parallel flow, shear stress (τ\tau) is directly proportional to the velocity gradient (shear rate γ˙\dot{\gamma}):

τyx=−μdvxdy=μγ˙\tau_{yx} = -\mu \frac{dv_x}{dy} = \mu \dot{\gamma}

Where:

  • τyx\tau_{yx} = shear stress parallel to the xx-plane (N/m2\text{N/m}^2 or Pa\text{Pa}, lbf/ft2\text{lbf/ft}^2).
  • γ˙=∣dvx/dy∣\dot{\gamma} = |dv_x/dy| = shear rate (s−1\text{s}^{-1}).
  • μ\mu = dynamic (absolute) viscosity.
          Moving Plate (Area A, Velocity V) ------> Force F
          ===================================================
          Fluid Layer: Velocity Gradient dv/dy (Shear Rate)
          ---------------------------------------------------
          Stationary Plate (v = 0)
          ===================================================
          Shear Stress: tau = F / A = mu * (dv/dy)

Dynamic Viscosity Units and Conversions

  • SI Unit: Pa⋅s=kg/(m⋅s)=N⋅s/m2\text{Pa}\cdot\text{s} = \text{kg}/(\text{m}\cdot\text{s}) = \text{N}\cdot\text{s/m}^2.
  • CGS Unit: Poise (P)=g/(cm⋅s)=0.10 Pa⋅s\text{Poise (P)} = \text{g}/(\text{cm}\cdot\text{s}) = 0.10\text{ Pa}\cdot\text{s}. The industrial sub-unit is the centipoise (cP): 1.0 cP=10−2 P=10−3 Pa⋅s=1.0 mPa⋅s1.0\text{ cP} = 10^{-2}\text{ P} = 10^{-3}\text{ Pa}\cdot\text{s} = 1.0\text{ mPa}\cdot\text{s} (Convenient reference: Liquid water at 20.0∘C20.0^\circ\text{C} has μ=1.002 cP≈1.0 cP\mu = 1.002\text{ cP} \approx 1.0\text{ cP}).
  • US Customary Units: lbm/(ft⋅s)\text{lbm}/(\text{ft}\cdot\text{s}), lbm/(ft⋅hr)\text{lbm}/(\text{ft}\cdot\text{hr}), and lbf⋅s/ft2\text{lbf}\cdot\text{s/ft}^2: 1.0 cP=6.7197×10−4 lbm/(ft⋅s)=2.4191 lbm/(ft⋅hr)=2.0885×10−5 lbf⋅s/ft21.0\text{ cP} = 6.7197 \times 10^{-4}\text{ lbm}/(\text{ft}\cdot\text{s}) = 2.4191\text{ lbm}/(\text{ft}\cdot\text{hr}) = 2.0885 \times 10^{-5}\text{ lbf}\cdot\text{s/ft}^2

Kinematic Viscosity (ν\nu)

Kinematic viscosity is the ratio of dynamic viscosity to fluid density, representing the momentum diffusivity of the fluid:

ν≡μρ\nu \equiv \frac{\mu}{\rho}
  • SI Unit: m2/s\text{m}^2/\text{s}.
  • CGS Unit: Stokes (St)=cm2/s=10−4 m2/s\text{Stokes (St)} = \text{cm}^2/\text{s} = 10^{-4}\text{ m}^2/\text{s}. The standard sub-unit is the centistokes (cSt): 1.0 cSt=10−2 St=10−6 m2/s=1.0 mm2/s1.0\text{ cSt} = 10^{-2}\text{ St} = 10^{-6}\text{ m}^2/\text{s} = 1.0\text{ mm}^2/\text{s} (Reference: Pure water at 20.0∘C20.0^\circ\text{C} has ν=1.002/0.9982≈1.004 cSt\nu = 1.002 / 0.9982 \approx 1.004\text{ cSt}).
  • US Customary Unit: ft2/s\text{ft}^2/\text{s}: 1.0 cSt=1.0764×10−5 ft2/s1.0\text{ cSt} = 1.0764 \times 10^{-5}\text{ ft}^2/\text{s}
  • Saybolt Universal Seconds (SUS): In older petroleum specifications, efflux time from a calibrated Saybolt viscometer is reported in SUS (tt in seconds at 100∘F100^\circ\text{F} or 210∘F210^\circ\text{F}): ν (cSt)=0.226t−195t(for 32≤t≤100 SUS)\nu\text{ (cSt)} = 0.226 t - \frac{195}{t} \quad (\text{for } 32 \le t \le 100\text{ SUS}) ν (cSt)=0.220t−135t≈0.216t(for t>100 SUS)\nu\text{ (cSt)} = 0.220 t - \frac{135}{t} \approx 0.216 t \quad (\text{for } t > 100\text{ SUS})

3. Rheological Classifications: Newtonian vs. Non-Newtonian Fluids

Fluids are classified by how their shear stress responds to imposed shear rate:

   Shear Stress (tau)
     ^
     |        / Dilatant (Shear-Thickening, n > 1)
     |       /   
     |      /      / Newtonian (n = 1, Constant mu)
     |     /      / 
     |    /      /        / Pseudoplastic (Shear-Thinning, n < 1)
     |   /      /        / 
     |  /      /        /
   tau0 +-----+--------+---------- Bingham Plastic (Yield Stress tau0)
     | /     /        /
     |/     /        /
     +-----------------------------------> Shear Rate (gamma_dot)

1. Newtonian Fluids

Newtonian fluids have a constant dynamic viscosity independent of shear rate or duration of shear. Examples include water, air, light hydrocarbons, simple alcohols, and benzene.

2. Ostwald-de Waele Power Law Model

For non-Newtonian fluids lacking yield stress, the power law model relates shear stress to shear rate:

τ=Kγ˙n\tau = K \dot{\gamma}^n

Where:

  • KK = flow consistency index (Pa⋅sn\text{Pa}\cdot\text{s}^n or lbf⋅sn/ft2\text{lbf}\cdot\text{s}^n/\text{ft}^2).
  • nn = flow behavior index (dimensionless).

The apparent viscosity (μapp\mu_{\text{app}}) is the effective viscosity at a specific local shear rate:

μapp=τγ˙=Kγ˙n−1\mu_{\text{app}} = \frac{\tau}{\dot{\gamma}} = K \dot{\gamma}^{n-1}
  • Pseudoplastic (Shear-Thinning, n<1n < 1): Apparent viscosity decreases as shear rate increases. Molecular entanglements uncoil and align parallel to the flow streamlines. Examples: polymer melts, latex paint, fermentation broths, blood, paper pulp.
  • Dilatant (Shear-Thickening, n>1n > 1): Apparent viscosity increases as shear rate increases. High shear disrupts the packing of concentrated suspensions, forcing fluid into void spaces and increasing solid-solid interparticle friction. Examples: concentrated cornstarch suspensions (oobleck), wet beach sand, high-solids titanium dioxide slurries.

3. Bingham Plastics

Bingham plastics behave as rigid solids until an external yield stress (τ0\tau_0) is exceeded, after which they flow with a constant plastic viscosity (μp\mu_p or μ∞\mu_\infty):

τ=τ0+μpγ˙(for ∣τ∣>τ0)\tau = \tau_0 + \mu_p \dot{\gamma} \quad (\text{for } |\tau| > \tau_0) γ˙=0(for ∣τ∣≤τ0)\dot{\gamma} = 0 \quad (\text{for } |\tau| \le \tau_0)

Examples include drilling muds, sewage sludge, toothpastes, greases, and mayonnaise.

4. Time-Dependent Rheology

  • Thixotropic: Apparent viscosity decreases reversibly over time under constant, sustained shear rate (e.g., non-drip paints, drilling muds after standing).
  • Rheopectic: Apparent viscosity increases reversibly over time under constant, sustained shear rate (e.g., gypsum slurries, bentonite clay pastes).

4. Temperature and Pressure Dependencies of Viscosity

Liquid Viscosity vs. Temperature: The Andrade / Arrhenius Equation

In liquids, molecules are closely packed in mutual potential energy wells. Momentum transfer occurs via short-range attractive intermolecular forces and molecular cage jumps into adjacent voids (free volume). Rising temperature increases thermal expansion, expanding intermolecular distances and providing thermal activation energy to overcome attractive cages. Consequently, liquid viscosity decreases exponentially with increasing temperature:

ln⁡(μL)=A+BT  ⟺  μL(T)=A′exp⁡(EaRT)\ln(\mu_L) = A + \frac{B}{T} \iff \mu_L(T) = A' \exp\left( \frac{E_a}{R T} \right)

Where TT is absolute temperature (K\text{K} or ∘R^\circ\text{R}) and EaE_a is the activation energy for viscous flow. For broad temperature spans, the three-parameter Vogel-Fulcher-Tammann (VFT) correlation is applied:

ln⁡(μL)=A+BT−T0\ln(\mu_L) = A + \frac{B}{T - T_0}

Gas Viscosity vs. Temperature: Kinetic Theory & Sutherland's Law

In low-pressure gases, molecules are separated by distances much greater than their molecular diameters. Intermolecular attractive forces are negligible. Momentum transport occurs exclusively by the physical translation of gas molecules carrying momentum across parallel flow streamlines through collisions. Kinetic theory shows that the mean molecular thermal velocity is:

vˉ=8RTπM∝T\bar{v} = \sqrt{\frac{8 R T}{\pi M}} \propto \sqrt{T}

Because hotter gas molecules travel faster and collide more frequently, gas viscosity increases with increasing temperature:

μG∝MT\mu_G \propto \sqrt{M T}

According to Chapman-Enskog kinetic theory for dilute gases:

μG=2.6693×10−5MTσ2Ωv(poise)\mu_G = 2.6693 \times 10^{-5} \frac{\sqrt{M T}}{\sigma^2 \Omega_v} \quad (\text{poise})

Where σ\sigma is the collision diameter (A˚\text{Å}) and Ωv\Omega_v is the dimensionless collision integral (which varies weakly with kBT/ϵk_B T / \epsilon).

For engineering calculations across wide temperature ranges, Sutherland's formula incorporates intermolecular attractions via an empirical Sutherland constant (SS in K\text{K}):

μG(T)=μ0(TT0)3/2T0+ST+S\mu_G(T) = \mu_0 \left( \frac{T}{T_0} \right)^{3/2} \frac{T_0 + S}{T + S}

Pressure Dependence of Viscosity

  • Liquids: Because liquids are virtually incompressible, viscosity is nearly independent of pressure from vacuum up to 20−50 bar20-50\text{ bar}. At extreme pressures (>100−1000 bar> 100-1000\text{ bar}), free volume is compressed, causing viscosity to increase exponentially.
  • Gases: At low to moderate pressures (P<10 barP < 10\text{ bar}), gas viscosity is independent of pressure (as predicted by Maxwell, because gas density increases linearly while molecular mean free path decreases proportionally, cancelling out). At high pressures (Pr>1P_r > 1), dense gases and supercritical fluids experience molecular clustering, causing viscosity to increase sharply toward liquid-like magnitudes.

5. Summary Comparison Table: Density and Viscosity Principles

Property / ParameterLiquid PhaseGas Phase (Low to Moderate PP)Dense / Supercritical Fluid
Density (ρ)500−1500 kg/m3500 - 1500\text{ kg/m}^3; modeled via Rackett eq.0.5−5 kg/m30.5 - 5\text{ kg/m}^3; ρ=PM/(ZRT)\rho = P M / (Z R T)100−800 kg/m3100 - 800\text{ kg/m}^3; cubic EOS / departure functions
Effect of Temperature on ρDecreases moderately with TTDecreases inversely with TT (ρ∝1/T\rho \propto 1/T)Decreases sharply near critical point
Effect of Pressure on ρNearly incompressible (dρ/dP≈0d\rho/dP \approx 0)Increases linearly with PP (ρ∝P\rho \propto P)Highly compressible (Z≪1Z \ll 1)
Dynamic Viscosity (μ)0.2−1000+ cP0.2 - 1000+\text{ cP}0.01−0.03 cP0.01 - 0.03\text{ cP} (10−30  μPa⋅s10 - 30\;\mu\text{Pa}\cdot\text{s})0.05−0.2 cP0.05 - 0.2\text{ cP}
Effect of Temperature on μDecreases exponentially (ln⁡μ=A+B/T\ln \mu = A + B/T)Increases (μ∝T1/2\mu \propto T^{1/2} or Sutherland)Increases at low PrP_r, decreases at high PrP_r
Effect of Pressure on μNegligible up to ≈50 bar\approx 50\text{ bar}Negligible up to ≈10 bar\approx 10\text{ bar}Increases significantly with PP
Primary MechanismIntermolecular cohesive cage jumpingIntermolecular ballistic momentum exchangeCombined collisional & dense fluid clustering

6. Comprehensive Worked Numerical Example

Problem Statement

A chemical facility processes an organic process stream and a drilling mud slurry. Solve the following three engineering evaluations:

  1. Crude Fraction Characterization: A petroleum condensate has an API gravity of 32.0∘API32.0^\circ\text{API} at 60.0∘F60.0^\circ\text{F}. Determine its specific gravity SG60/60∘FSG_{60/60^\circ\text{F}}, mass density ρ\rho in lbm/ft3\text{lbm/ft}^3, and mass flow rate m˙\dot{m} in lbm/hr\text{lbm/hr} for a pipeline transporting 500.0 gpm500.0\text{ gpm}.
  2. Rackett Saturated Liquid Density: Saturated liquid isobutane (M=58.12 kg/kmolM = 58.12\text{ kg/kmol}) is stored at 300.0 K300.0\text{ K}. Given Tc=407.8 KT_c = 407.8\text{ K}, Pc=3640 kPaP_c = 3640\text{ kPa}, and ZRA=0.2829Z_{RA} = 0.2829, calculate the saturated molar volume VsatV_{\text{sat}} in m3/kmol\text{m}^3/\text{kmol} and mass density ρsat\rho_{\text{sat}} in kg/m3\text{kg/m}^3.
  3. Power-Law Slurry Flow: A shear-thinning mineral slurry flows through a D=0.100 mD = 0.100\text{ m} ID pipe at an average velocity of Vavg=1.50 m/sV_{\text{avg}} = 1.50\text{ m/s}. The slurry obeys the Ostwald-de Waele model with K=0.800 Pa⋅snK = 0.800\text{ Pa}\cdot\text{s}^n and n=0.600n = 0.600. Determine the wall shear rate γ˙w\dot{\gamma}_w, wall shear stress τw\tau_w, and apparent viscosity μapp,w\mu_{\text{app},w} at the pipe wall in cP\text{cP}.

Step 1: Petroleum Condensate Characterization

From the API gravity definition:

SG60/60∘F=141.5∘API+131.5=141.532.0+131.5=141.5163.5=0.86544SG_{60/60^\circ\text{F}} = \frac{141.5}{^\circ\text{API} + 131.5} = \frac{141.5}{32.0 + 131.5} = \frac{141.5}{163.5} = \mathbf{0.86544}

Mass density at 60∘F60^\circ\text{F}:

ρ=SG×ρwater(60∘F)=0.86544×62.366 lbm/ft3=53.974 lbm/ft3\rho = SG \times \rho_{\text{water}}(60^\circ\text{F}) = 0.86544 \times 62.366\text{ lbm/ft}^3 = \mathbf{53.974\text{ lbm/ft}^3}

Volumetric flow rate conversion (1 ft3=7.4805 gal1\text{ ft}^3 = 7.4805\text{ gal}):

Q=500.0 gpm×1 ft3/s448.83 gpm=1.1140 ft3/s=66.840 ft3/minQ = 500.0\text{ gpm} \times \frac{1\text{ ft}^3/\text{s}}{448.83\text{ gpm}} = 1.1140\text{ ft}^3/\text{s} = 66.840\text{ ft}^3/\text{min} m˙=Q⋅ρ=(1.1140 ft3/s)×(53.974 lbm/ft3)×3600 s/hr=2.1645×105 lbm/hr\dot{m} = Q \cdot \rho = (1.1140\text{ ft}^3/\text{s}) \times (53.974\text{ lbm/ft}^3) \times 3600\text{ s/hr} = \mathbf{2.1645 \times 10^5\text{ lbm/hr}}

Step 2: Saturated Isobutane via Rackett Equation

Compute reduced temperature:

Tr=TTc=300.0 K407.8 K=0.73565T_r = \frac{T}{T_c} = \frac{300.0\text{ K}}{407.8\text{ K}} = 0.73565 1−Tr=1−0.73565=0.264351 - T_r = 1 - 0.73565 = 0.26435

Evaluate the exponent bracket:

(1−Tr)2/7=(0.26435)0.285714=0.68377(1 - T_r)^{2/7} = (0.26435)^{0.285714} = 0.68377 Exponent=1+(1−Tr)2/7=1+0.68377=1.68377\text{Exponent} = 1 + (1 - T_r)^{2/7} = 1 + 0.68377 = 1.68377

Evaluate ZRAExponentZ_{RA}^{\text{Exponent}}:

ZRA1.68377=(0.2829)1.68377=exp⁡(1.68377×ln⁡(0.2829))=exp⁡(1.68377×(−1.26267))=exp⁡(−2.12604)=0.11931Z_{RA}^{1.68377} = (0.2829)^{1.68377} = \exp(1.68377 \times \ln(0.2829)) = \exp(1.68377 \times (-1.26267)) = \exp(-2.12604) = 0.11931

Calculate critical molar volume ratio:

RTcPc=(8.3145 kPa⋅m3/(kmol⋅K))×(407.8 K)3640 kPa=3390.653640=0.93150 m3/kmol\frac{R T_c}{P_c} = \frac{(8.3145\text{ kPa}\cdot\text{m}^3/(\text{kmol}\cdot\text{K})) \times (407.8\text{ K})}{3640\text{ kPa}} = \frac{3390.65}{3640} = 0.93150\text{ m}^3/\text{kmol}

Compute saturated molar volume and mass density:

Vsat=0.93150×0.11931=0.11114 m3/kmol=111.14 cm3/molV_{\text{sat}} = 0.93150 \times 0.11931 = \mathbf{0.11114\text{ m}^3/\text{kmol}} = 111.14\text{ cm}^3/\text{mol} ρsat=MVsat=58.12 kg/kmol0.11114 m3/kmol=522.9 kg/m3\rho_{\text{sat}} = \frac{M}{V_{\text{sat}}} = \frac{58.12\text{ kg/kmol}}{0.11114\text{ m}^3/\text{kmol}} = \mathbf{522.9\text{ kg/m}^3}

Step 3: Non-Newtonian Slurry Pipe Hydraulics

For fully developed laminar pipe flow of a power-law fluid, the wall shear rate is given by the Rabinowitsch-Mooney equation:

γ˙w=(3n+14n)(8VavgD)\dot{\gamma}_w = \left( \frac{3n + 1}{4n} \right) \left( \frac{8 V_{\text{avg}}}{D} \right) 3n+14n=3(0.600)+14(0.600)=2.8002.400=1.1667\frac{3n + 1}{4n} = \frac{3(0.600) + 1}{4(0.600)} = \frac{2.800}{2.400} = 1.1667 8VavgD=8×1.50 m/s0.100 m=120.0 s−1\frac{8 V_{\text{avg}}}{D} = \frac{8 \times 1.50\text{ m/s}}{0.100\text{ m}} = 120.0\text{ s}^{-1} γ˙w=1.1667×120.0 s−1=140.0 s−1\dot{\gamma}_w = 1.1667 \times 120.0\text{ s}^{-1} = \mathbf{140.0\text{ s}^{-1}}

Compute wall shear stress:

τw=K(γ˙w)n=0.800×(140.0)0.600=0.800×19.394=15.515 Pa\tau_w = K (\dot{\gamma}_w)^n = 0.800 \times (140.0)^{0.600} = 0.800 \times 19.394 = \mathbf{15.515\text{ Pa}}

Compute apparent viscosity at the pipe wall:

μapp,w=τwγ˙w=15.515 Pa140.0 s−1=0.11082 Pa⋅s=110.8 cP\mu_{\text{app},w} = \frac{\tau_w}{\dot{\gamma}_w} = \frac{15.515\text{ Pa}}{140.0\text{ s}^{-1}} = 0.11082\text{ Pa}\cdot\text{s} = \mathbf{110.8\text{ cP}}

(Notice that without shear, the fluid would be much thicker; at γ˙=1.0 s−1\dot{\gamma} = 1.0\text{ s}^{-1}, μapp=0.800 Pa⋅s=800 cP\mu_{\text{app}} = 0.800\text{ Pa}\cdot\text{s} = 800\text{ cP}. Shearing reduces viscosity by over 86%86\%).


7. Critical PE Exam Traps & Pitfalls

Warning

Trap 1: Gas Viscosity vs. Liquid Viscosity Temperature Trends
The most heavily tested conceptual trap on the PE Chemical exam is the opposite effect of temperature on gas versus liquid viscosity. When temperature rises, liquid viscosity decreases (cohesion drops), but gas viscosity increases (molecular collisions increase). Applying ln⁡μ=A+B/T\ln \mu = A + B/T to a gas or assuming gas viscosity drops with heat leads to immediate error.

Warning

Trap 2: Dynamic vs. Kinematic Viscosity Units
Converting centipoise directly to centistokes without dividing by density is a major error source: ν (cSt)=μ (cP)/SG\nu\text{ (cSt)} = \mu\text{ (cP)} / SG. If an oil has μ=20 cP\mu = 20\text{ cP} and SG=0.80SG = 0.80, ν=20/0.80=25 cSt\nu = 20 / 0.80 = 25\text{ cSt}, NOT 20 cSt20\text{ cSt}. In English units, remember that 1 cP=6.7197×10−4 lbm/(ft⋅s)1\text{ cP} = 6.7197 \times 10^{-4}\text{ lbm}/(\text{ft}\cdot\text{s}), while kinematic viscosity is in ft2/s\text{ft}^2/\text{s}.

Warning

Trap 3: Inverting the API Gravity Equation
Because ∘API^\circ\text{API} is inversely related to specific gravity, higher ∘API^\circ\text{API} means lighter crude. Candidates sometimes erroneously associate high API gravity with heavy, viscous oils. Pure water has an API gravity of 10.0∘API10.0^\circ\text{API}; crudes that float on water always have ∘API>10.0^\circ\text{API} > 10.0.

Test Your Knowledge

A petroleum storage facility receives a batch of light sweet crude oil rated at 34.0°API at 60.0°F. What is the specific gravity SG_60/60F, the mass density in lbm/ft³, and the total mass contained in a 10,000-barrel storage tank?

A

SG = 0.8550, rho = 53.32 lbm/ft³, Mass = 2.994 × 10⁶ lbm

B

SG = 1.170, rho = 72.97 lbm/ft³, Mass = 4.097 × 10⁶ lbm

C

SG = 0.8550, rho = 62.37 lbm/ft³, Mass = 3.502 × 10⁶ lbm

D

SG = 0.7630, rho = 47.59 lbm/ft³, Mass = 2.672 × 10⁶ lbm

Test Your Knowledge

A concentrated non-Newtonian polymer solution behaves as an Ostwald-de Waele power-law fluid with flow consistency index K = 4.50 Pa·sⁿ and flow behavior index n = 0.40. When subjected to a steady shear rate of 250 s⁻¹ in a rotational rheometer, what are the shear stress and apparent dynamic viscosity of the solution?

A

Shear stress = 1,125 Pa, Apparent viscosity = 4,500 cP

B

Shear stress = 41.0 Pa, Apparent viscosity = 163.9 cP

C

Shear stress = 25.4 Pa, Apparent viscosity = 101.6 cP

D

Shear stress = 82.0 Pa, Apparent viscosity = 327.7 cP

Test Your Knowledge

An engineer is designing a heat exchanger where a low-pressure gas and a hydrocarbon liquid are both heated from 300 K to 600 K at a constant pressure of 1 atm. Based on transport phenomena principles, how do the dynamic viscosities of the gas and liquid respond to this temperature increase?

A

The gas viscosity decreases by approximately 41.4%, while the liquid viscosity increases exponentially.

B

The gas viscosity remains constant because pressure is 1 atm, while the liquid viscosity decreases linearly.

C

The gas viscosity increases by approximately 41.4% (proportional to T^(1/2)), while the liquid viscosity decreases exponentially due to thermal expansion weakening intermolecular cohesive forces.

D

Both gas and liquid dynamic viscosities increase by 41.4% because thermal energy accelerates molecular motion across all fluid phases.

Sections you finish are checked off in the contents.